TY - DATA
T1 - Effect of Bondline Thickness on Fatigue Crack Growth in FM94
PY - 2016/06/08
AU - John-Alan Pascoe
AU - A. M.K. H. (Ali) Al Amery
AU - N. (Nicola) Zavatta
UR - https://data.4tu.nl/articles/dataset/Effect_of_Bondline_Thickness_on_Fatigue_Crack_Growth_in_FM94/12680906/1
DO - 10.4121/uuid:1495c951-33e2-43ab-9f41-5ed3b57ba02f
KW - Adhesive bond
KW - Aerospace engineering
KW - Bonded joint
KW - Double Cantilever Beam (DCB)
KW - Double cantilever beam
KW - Epoxy
KW - FM94
KW - Fatigue crack growth
KW - Glass-Fibre Reinforced Polymer (GFRP)
KW - Glass-fibre reinforced polymer
N2 - Fatigue crack growth experiments on aluminium-2024-T3 / FM94 epoxy / aluminium-2024-T3 bonded joint specimens in the double cantilever beam (DCB) configuration. Different adhesive thicknesses were tested.
Also contains data from fatigue crack growth experiments conducted on S2-glass / FM94 epoxy composite laminates again in the DCB configuration. Different fibre orientations were tested.

Included data are raw data: crack length, force, and displacement measurements, as well as processed data such as strain energy release rates and energy dissipation per cycle.
ER -